EP1348898A1 - Ansauggleitringdichtung mit axialen Dichtungszähnen - Google Patents

Ansauggleitringdichtung mit axialen Dichtungszähnen Download PDF

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Publication number
EP1348898A1
EP1348898A1 EP03251743A EP03251743A EP1348898A1 EP 1348898 A1 EP1348898 A1 EP 1348898A1 EP 03251743 A EP03251743 A EP 03251743A EP 03251743 A EP03251743 A EP 03251743A EP 1348898 A1 EP1348898 A1 EP 1348898A1
Authority
EP
European Patent Office
Prior art keywords
rotatable
seal
gas bearing
bearing face
annular
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP03251743A
Other languages
English (en)
French (fr)
Inventor
John C. Brauer
Robert J. Albers
Christopher C. Glynn
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of EP1348898A1 publication Critical patent/EP1348898A1/de
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J15/00—Sealings
    • F16J15/44—Free-space packings
    • F16J15/441—Free-space packings with floating ring
    • F16J15/442—Free-space packings with floating ring segmented
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations

Definitions

  • the present invention relates generally to aspirating face seals for rotor and stator assemblies and, more particularly, to a rotor and stator assembly with an aspirating face seal having seal teeth.
  • Aspirating face seals are used to minimize leakage through a gap between two components and from a higher pressure area to a lower pressure area. Such seals have been disclosed for use in rotating machinery, including, but not limited to, turbomachinery such as gas turbine engines used for power generation and for aircraft and marine propulsion. Aspirating face seals are designed to minimize leakage of a fluid such compressed air or combustion gases between a rotor and a stator in gas turbine engines.
  • FIG. 1 Illustrated in FIG. 1 and more particularly in FIG. 2 is a first exemplary embodiment of the face seal 40 of the present invention having non-rotatable annular radially inner and outer axially extending tooth rings 42 and 44, respectively.
  • the face seal 40 is designed to restrict leakage of the high pressure compressor discharge air 20 through the leakage path 45 from the relatively high pressure region 48 to the relatively low pressure region 46 at the juncture 49 between the rotatable turbine stage 22 and the stationary structure 58.
  • a face seal ring 60 is mounted on a non-rotatable axially translatable cylindrical piston 88 which is circumferentially continuous and axially movably supported on a stationary face seal support structure 52.
  • the face seal ring 60 exemplifies an axially movable non-rotatable engine member 61 of the present invention.
  • the face seal support structure 52 is fixed with respect to the stationary structure 58.
  • the radially inner and outer axially extending tooth rings 42 and 44 are mounted on the face seal ring 60 and extend radially outward from an axially facing generally planar non-rotatable gas bearing face surface 68 towards an axially facing generally planar rotatable substantially planar gas bearing face surface 62.
  • the face seal ring 60 is supported for axial movement with respect to the rotatable gas bearing face surface 62 which is on the side plate 34 that is mounted to the rotor disk 28.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mechanical Sealing (AREA)
  • Sealing Of Bearings (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
EP03251743A 2002-03-26 2003-03-20 Ansauggleitringdichtung mit axialen Dichtungszähnen Withdrawn EP1348898A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US106401 1998-06-29
US10/106,401 US6676369B2 (en) 2002-03-26 2002-03-26 Aspirating face seal with axially extending seal teeth

Publications (1)

Publication Number Publication Date
EP1348898A1 true EP1348898A1 (de) 2003-10-01

Family

ID=27804346

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03251743A Withdrawn EP1348898A1 (de) 2002-03-26 2003-03-20 Ansauggleitringdichtung mit axialen Dichtungszähnen

Country Status (3)

Country Link
US (1) US6676369B2 (de)
EP (1) EP1348898A1 (de)
JP (1) JP2003301950A (de)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1348834A2 (de) * 2002-03-26 2003-10-01 General Electric Company Rotorabdichtung für eine Turbine
EP2025876A2 (de) * 2007-08-17 2009-02-18 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
EP2025875A2 (de) 2007-08-17 2009-02-18 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
EP2025874A3 (de) * 2007-08-17 2011-05-18 United Technologies Corporation Hydrostatische Dichtung von einem Gasturbinentriebwerk und entsprechendes Gasturbinentriebwerk
FR2961283A1 (fr) * 2010-06-11 2011-12-16 Snecma Joint asservi par une difference de pression entre deux enceintes
US8105021B2 (en) 2007-08-20 2012-01-31 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
EP2803825A1 (de) * 2012-01-12 2014-11-19 Mitsubishi Heavy Industries, Ltd. Dichtungsstruktur für eine drehmaschine und gasturbine damit
EP3073060A1 (de) * 2015-03-19 2016-09-28 United Technologies Corporation Dichtungshalterungsstrukturen für turbomaschinen
US9765638B2 (en) 2012-01-12 2017-09-19 Mitsubishi Heavy Industries, Ltd. Assembling method of seal structure of rotary machine

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US8047767B2 (en) * 2005-09-28 2011-11-01 General Electric Company High pressure first stage turbine and seal assembly
US8608175B2 (en) * 2005-10-28 2013-12-17 United Technologies Corporation Mechanical face seal stop pin
US7976274B2 (en) * 2005-12-08 2011-07-12 General Electric Company Methods and apparatus for assembling turbine engines
US20070253809A1 (en) * 2006-05-01 2007-11-01 General Electric Company Methods and apparatus for assembling gas turbine engines
US20080018054A1 (en) * 2006-07-20 2008-01-24 General Electric Company Aspirating labyrinth seal
US7828513B2 (en) * 2006-10-05 2010-11-09 Pratt & Whitney Canada Corp. Air seal arrangement for a gas turbine engine
US20110229311A1 (en) * 2007-07-30 2011-09-22 Kripa Varanasi Seal assembly
US20090051120A1 (en) * 2007-08-23 2009-02-26 United Technologies Corp. Gas Turbine Engine Systems Involving Hydrostatic Face Seals
US7797941B2 (en) * 2007-10-26 2010-09-21 United Technologies Corporation Gas turbine engine systems involving hydrostatic face seals
US7946590B2 (en) * 2008-01-17 2011-05-24 United Technologies Corporation Face seal for gas turbine engine
US7984911B2 (en) * 2008-01-17 2011-07-26 United Technologies Corporation Face seal for gas turbine engine
US8167545B2 (en) * 2008-02-27 2012-05-01 United Technologies Corp. Self-balancing face seals and gas turbine engine systems involving such seals
US8070426B2 (en) * 2008-05-19 2011-12-06 Baker Hughes Incorporated System, method and apparatus for open impeller and diffuser assembly for multi-stage submersible pump
US20090304493A1 (en) * 2008-06-09 2009-12-10 General Electric Company Axially oriented shingle face seal for turbine rotor and related method
US8277172B2 (en) * 2009-03-23 2012-10-02 General Electric Company Apparatus for turbine engine cooling air management
US8142141B2 (en) * 2009-03-23 2012-03-27 General Electric Company Apparatus for turbine engine cooling air management
US8864443B2 (en) * 2010-07-14 2014-10-21 Hitachi, Ltd. Sealing device for steam turbines and method for controlling sealing device
US20130180256A1 (en) * 2012-01-17 2013-07-18 General Electric Company Turbine fuel nozzle assembly and method for operating a turbine
US9097350B2 (en) 2012-04-02 2015-08-04 United Technologies Corporation Axial non-contact seal
US20140010649A1 (en) * 2012-07-09 2014-01-09 United Technologies Corporation Mid-turbine frame hpt seal support meshing
US9328626B2 (en) * 2012-08-21 2016-05-03 United Technologies Corporation Annular turbomachine seal and heat shield
US9726031B2 (en) * 2012-09-28 2017-08-08 United Technologies Corporation Piston ring coated carbon seal
WO2014107161A1 (en) * 2013-01-04 2014-07-10 United Technologies Corporation Seal assembly for arranging between a stator and a rotor
US9291067B2 (en) 2013-11-11 2016-03-22 General Electric Company Rotary machine aspirating seal assembly and method of assembling the same
US9976420B2 (en) * 2015-07-23 2018-05-22 General Electric Company Aspirating seal assembly and method of assembling
US10107126B2 (en) * 2015-08-19 2018-10-23 United Technologies Corporation Non-contact seal assembly for rotational equipment
US9909438B2 (en) 2016-04-12 2018-03-06 United Technologies Corporation Hydrodynamic carbon face seal pressure booster
WO2017180682A1 (en) * 2016-04-14 2017-10-19 General Electric Company Anti-coning aspirating face seal
US10344602B2 (en) 2016-04-18 2019-07-09 General Electric Company Gas turbine engine transition duct and turbine center frame
US10428673B2 (en) 2016-05-02 2019-10-01 General Electric Company Aspirating face seal assembly and a method of operating the same
WO2017196563A1 (en) 2016-05-11 2017-11-16 General Electric Company Aspirating face seal tooth configuration
US10823184B2 (en) 2016-07-28 2020-11-03 General Electric Company Engine with face seal
US10359117B2 (en) * 2017-03-06 2019-07-23 General Electric Company Aspirating face seal with non-coiled retraction springs
US10329938B2 (en) 2017-05-31 2019-06-25 General Electric Company Aspirating face seal starter tooth abradable pocket
US10711629B2 (en) 2017-09-20 2020-07-14 Generl Electric Company Method of clearance control for an interdigitated turbine engine
US10458267B2 (en) 2017-09-20 2019-10-29 General Electric Company Seal assembly for counter rotating turbine assembly
US10563772B2 (en) 2017-11-13 2020-02-18 General Electric Company Seal assembly and an associated method thereof
US10781709B2 (en) * 2018-01-09 2020-09-22 General Electric Company Turbine engine with a seal
US11118469B2 (en) 2018-11-19 2021-09-14 General Electric Company Seal assembly for a turbo machine
US10968762B2 (en) 2018-11-19 2021-04-06 General Electric Company Seal assembly for a turbo machine
US10895324B2 (en) * 2018-11-27 2021-01-19 General Electric Company Aspirating face seal assembly for a rotary machine
US10900570B2 (en) * 2018-11-27 2021-01-26 General Electric Company Aspirating face seal assembly for a rotary machine
US11035253B2 (en) 2019-02-05 2021-06-15 Raytheon Technologies Corporation Face seal with damper
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

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US5975537A (en) * 1997-07-01 1999-11-02 General Electric Company Rotor and stator assembly configured as an aspirating face seal

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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1348834A3 (de) * 2002-03-26 2005-06-22 General Electric Company Rotorabdichtung für eine Turbine
EP1348834A2 (de) * 2002-03-26 2003-10-01 General Electric Company Rotorabdichtung für eine Turbine
US8109717B2 (en) 2007-08-17 2012-02-07 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
EP2025876A2 (de) * 2007-08-17 2009-02-18 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
EP2025875A2 (de) 2007-08-17 2009-02-18 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
EP2025874A3 (de) * 2007-08-17 2011-05-18 United Technologies Corporation Hydrostatische Dichtung von einem Gasturbinentriebwerk und entsprechendes Gasturbinentriebwerk
EP2025876A3 (de) * 2007-08-17 2011-05-18 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
EP2025875A3 (de) * 2007-08-17 2011-05-25 United Technologies Corporation Turbinendichtung und Sicherungsdichtung von einem Gasturbinentriebwerk und entsprechende Turbinenanordnung
US8109716B2 (en) 2007-08-17 2012-02-07 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with anti-fouling provisioning
US8105021B2 (en) 2007-08-20 2012-01-31 United Technologies Corp. Gas turbine engine systems involving hydrostatic face seals with integrated back-up seals
FR2961283A1 (fr) * 2010-06-11 2011-12-16 Snecma Joint asservi par une difference de pression entre deux enceintes
EP2803825A1 (de) * 2012-01-12 2014-11-19 Mitsubishi Heavy Industries, Ltd. Dichtungsstruktur für eine drehmaschine und gasturbine damit
EP2803825A4 (de) * 2012-01-12 2015-01-14 Mitsubishi Heavy Ind Ltd Dichtungsstruktur für eine drehmaschine und gasturbine damit
KR101531473B1 (ko) * 2012-01-12 2015-06-24 미츠비시 쥬고교 가부시키가이샤 회전 기계의 시일 구조 및 이를 구비한 가스 터빈
US9377109B2 (en) 2012-01-12 2016-06-28 Mitsubishi Heavy Industries, Ltd. Seal structure of rotary machine and gas turbine equipped with same
US9765638B2 (en) 2012-01-12 2017-09-19 Mitsubishi Heavy Industries, Ltd. Assembling method of seal structure of rotary machine
EP3073060A1 (de) * 2015-03-19 2016-09-28 United Technologies Corporation Dichtungshalterungsstrukturen für turbomaschinen
US9828881B2 (en) 2015-03-19 2017-11-28 United Technologies Corporation Seal support structures for turbomachines

Also Published As

Publication number Publication date
JP2003301950A (ja) 2003-10-24
US20030185669A1 (en) 2003-10-02
US6676369B2 (en) 2004-01-13

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